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AN4-52A

Aeronautical Standard Machine Bolt

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Description

Airframe Bolt

Specifications

Country of Origin USA
Drilling Undrilled Head
Fastener Length 5.281
Features Provided Finished head
Grip 4 13/16 in
Grip Length 4 13/16, 4.812
Hardness Rating 26.0 rockwell c minimum and 32.0 rockwell c maximum
Head Height 0.140 inches minimum and 0.172 inches maximum
Head Style Hexagon Head
Head Type Hexagon
Industry Standards/Certification AN4
Length 5 1/4, 5 9/32 in
Material Steel
Material Specification Mil-s-5626 mil spec 1st material response or mil-s-6049 mil spec 2nd material response or mil-s-6050 mil spec 3rd material response or mil-s-6098 mil spec 4th material response or mil-s-6758 mil spec 5th material response or mil-s-8695 mil spec 6th material response
Min. Tensile Strength (psi) 125000 pounds per square inch
NIIN 00-151-1098
NSN 5306-00-151-1098
Nominal Length 5 9/32
Surface Treatment Cadmium and chromate
Surface Treatment Specification Qq-p-416 ty 2 cl 3 fed spec all treatment responses
Thread Class 3a
Thread Diameter 0.250
Thread Direction Right-hand
Thread Length 0.469 inches minimum
Thread Qty 28
Thread Qty Per Inch (tpi) 28
Thread Series Designator UNF
Thread Size 1/4-28
Weight 0.08 lb
Width Between Flats 0.428 inches minimum and 0.440 inches maximum

Cross-reference

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Catalog data updated 2026-07-05. Report a data error